JPS6217114B2 - - Google Patents
Info
- Publication number
- JPS6217114B2 JPS6217114B2 JP55122947A JP12294780A JPS6217114B2 JP S6217114 B2 JPS6217114 B2 JP S6217114B2 JP 55122947 A JP55122947 A JP 55122947A JP 12294780 A JP12294780 A JP 12294780A JP S6217114 B2 JPS6217114 B2 JP S6217114B2
- Authority
- JP
- Japan
- Prior art keywords
- voltage
- triangular wave
- wave voltage
- angle
- retard
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 238000000034 method Methods 0.000 description 6
- 239000003990 capacitor Substances 0.000 description 5
- 238000010586 diagram Methods 0.000 description 4
- 230000000630 rising effect Effects 0.000 description 4
- 230000000979 retarding effect Effects 0.000 description 3
- 230000003321 amplification Effects 0.000 description 2
- 230000010354 integration Effects 0.000 description 2
- 238000003199 nucleic acid amplification method Methods 0.000 description 2
- 230000004907 flux Effects 0.000 description 1
- 230000005415 magnetization Effects 0.000 description 1
- 230000035699 permeability Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02P—IGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINES; TESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES
- F02P5/00—Advancing or retarding ignition; Control therefor
- F02P5/04—Advancing or retarding ignition; Control therefor automatically, as a function of the working conditions of the engine or vehicle or of the atmospheric conditions
- F02P5/145—Advancing or retarding ignition; Control therefor automatically, as a function of the working conditions of the engine or vehicle or of the atmospheric conditions using electrical means
- F02P5/155—Analogue data processing
- F02P5/1553—Analogue data processing by determination of elapsed angle with reference to a particular point on the motor axle, dependent on specific conditions
- F02P5/1556—Analogue data processing by determination of elapsed angle with reference to a particular point on the motor axle, dependent on specific conditions using a stepped control, dependent on speed
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/40—Engine management systems
Landscapes
- Engineering & Computer Science (AREA)
- Signal Processing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Electrical Control Of Ignition Timing (AREA)
Description
【発明の詳細な説明】
本発明はエンジン用無接点点火装置に係り、特
にエンジン回転速度の高い領域で点火位置を遅ら
せる特性を有するものに関する。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a non-contact ignition device for an engine, and particularly to one having a characteristic of delaying the ignition position in a region of high engine rotational speed.
エンジン用無接点点火装置として、第１図イに
示すように、最大進角位置Ｂから進角設定用偏倚
電圧V1分だけ垂直に立ち上がり、そこから最小
進角位置Ａまで所定の傾斜角をもつて立ち上がる
進角設定用の第１の三角波電圧Ｘと、最小進角位
置Ａから最大進角位置Ｂまで所定の傾斜角をもつ
て立ち上がり、それ以後最小進角位置Ａまでは平
担となる回転速度に応じた第２の三角波電圧Ｙを
作り、これら第１、第２の三角波電圧Ｘ，Ｙを組
合わせて、第１図ロに示すような波形を作り、そ
の立ち上がり点Ｃつまり第１、第２の三角波電圧
Ｘ，Ｙの交点を点火位置とするものが、例えば特
開昭55−10056号公報に見られるように提案され
ている。 As a non-contact ignition system for an engine, as shown in Figure 1A, the bias voltage for setting the advance angle rises vertically by 1 minute from the maximum advance angle position B, and then moves at a predetermined inclination angle from there to the minimum advance angle position A. The first triangular wave voltage X for setting the advance angle rises with a predetermined inclination angle from the minimum advance angle position A to the maximum advance angle position B, and thereafter remains flat until the minimum advance angle position A. A second triangular wave voltage Y corresponding to the rotational speed is created, and the first and second triangular wave voltages X and Y are combined to create a waveform as shown in Figure 1B, and its rising point C, that is, the first , a system in which the ignition position is the intersection of the second triangular wave voltages X and Y has been proposed, as can be seen, for example, in Japanese Patent Laid-Open No. 10056/1983.
この装置では、最小進角位置Ａから次の最小進
角位置Ａまでが１サイクルであり、エンジン回転
速度が高くなる程、１サイクルの時間が短かくな
るため、第２の三角波電圧Ｙの平担部の電圧V2
は低くなる。その結果、第２図のような点火位置
の進角特性が得られる。 In this device, the time from the minimum advance angle position A to the next minimum advance angle position A is one cycle, and the higher the engine speed, the shorter the time for one cycle. Part voltage V 2
becomes lower. As a result, the ignition position advance characteristic as shown in FIG. 2 is obtained.
即ち、エンジン回転速度が低く、第２の三角波
電圧Ｙの平担部の電圧V2が第１の三角波電圧Ｘ
の最大値より大きい領域では、第１図ロのよう
な波形が得られないため、点火位置は始動時点火
位置つまり最小進角位置Ａに固定され、一定であ
る。これより回転速度が上昇し、第２の三角波電
圧Ｙの平担部の電圧V2が小さくなつて第１の三
角波電圧Ｘの傾斜部と交差する領域では、第１
図ロのような波形が得られ、回転速度の上昇に応
じて点火位置Ｃは進角する。さらに回転速度が上
昇し、上記平担部の電圧V2が第１の三角波電圧
Ｘの進角設定用偏倚電圧V1より小さくなる領域
では、点火位置は最大進角位置に達し、回転速
度に関係なく一定となる。 That is, when the engine speed is low, the voltage V 2 of the flat part of the second triangular wave voltage Y is equal to the first triangular wave voltage X.
In a region larger than the maximum value of , the waveform shown in FIG. As the rotation speed increases from this point, the voltage V 2 at the flat part of the second triangular wave voltage Y becomes smaller, and in the region where it crosses the slope part of the first triangular wave voltage X, the first
A waveform as shown in Figure (B) is obtained, and the ignition position C advances as the rotational speed increases. In a region where the rotation speed further increases and the voltage V 2 of the flat portion becomes smaller than the lead angle setting bias voltage V 1 of the first triangular wave voltage X, the ignition position reaches the maximum advance position and the rotation speed increases. It remains constant regardless.
ところで、２サイクルエンジンは、点火位置を
最大進角位置に保つたまま高速域で運転すると出
力が低下する傾向があるため、高速域では逆に点
火位置を遅角させる必要がある。しかし、上述の
装置では高速域において点火位置を遅角させるこ
とはできない。 By the way, when a two-stroke engine is operated in a high speed range while keeping the ignition position at the maximum advance position, the output tends to decrease, so it is necessary to retard the ignition position in the high speed range. However, the above-mentioned device cannot retard the ignition position in a high speed range.
従来、高速域で点火位置を遅角させるものとし
ては、点火信号発電機の出力波形を変化させる方
法が知られている。この方法は、低中速域では点
火信号発電機の出力波形とそのまま点火信号とし
て使用し、高速域では点火信号発電機の負荷イン
ピーダンスをトランジスタを用いて大きくし、出
力波形を小さくすることにより点火位置を遅角さ
せるというものである。 Conventionally, a method of changing the output waveform of an ignition signal generator is known as a method for retarding the ignition position in a high-speed range. In this method, the output waveform of the ignition signal generator is used as the ignition signal in the low-to-medium speed range, and in the high-speed range, the load impedance of the ignition signal generator is increased using a transistor and the output waveform is made smaller. This is to retard the position.
しかし、この方法は、点火信号発電機の負荷イ
ンピーダンスを変化させることによつてコイルに
鎖交する磁束を変化させ、もつて出力波形を変化
させるという磁気的な手段を利用しているため、
例えば温度変化による磁石の透磁率の変化あるい
は磁石の着磁量の変化等によつて出力波形が変化
する傾向があり、さらにトランジスタの能動領域
を使用している関係からも、精度、温度特性が悪
いという欠点がある。 However, this method uses magnetic means to change the magnetic flux linking the coil by changing the load impedance of the ignition signal generator, thereby changing the output waveform.
For example, the output waveform tends to change due to changes in the magnetic permeability of the magnet due to temperature changes or changes in the amount of magnetization of the magnet, and furthermore, since the active area of the transistor is used, accuracy and temperature characteristics may vary. It has the disadvantage of being bad.
また、４サイクルエンジンは、高速域では点火
位置を遅角させない方がエンジン出力を大きくで
きるが、最近ではエンジン性能が向上し、エンジ
ン出力が出過ぎて過回転となり、クランクシヤフ
トを破損する等のおそれがあるため、ある回転速
度以上になつたら回転速度が上がらないように点
火位置を遅角させることが必要となつてきてい
る。 In addition, in a 4-cycle engine, engine output can be increased by not retarding the ignition position in the high-speed range, but recently, engine performance has improved, and there is a risk of over-revving the engine and damaging the crankshaft. Therefore, it has become necessary to retard the ignition position to prevent the rotational speed from increasing once the rotational speed exceeds a certain level.
本発明の目的は、上記のような従来技術の欠点
をなくし、電子回路を用いた制御により、高速域
で精度よく点火位置を遅角させることのできるエ
ンジン用無接点点火装置を提供するにある。 An object of the present invention is to eliminate the drawbacks of the prior art as described above and to provide a non-contact ignition device for an engine that is capable of accurately retarding the ignition position in a high speed range by control using an electronic circuit. .
この目的を達成するため、本発明は、進角設定
用の第１の三角波電圧と回転速度に応じた第２の
三角波電圧の交点を求め、この交点を点火位置と
するエンジン用無接点点火装置において、エンジ
ン回転速度が高い領域で回転速度に応じた遅角設
定用電圧を発生する手段を設け、この遅角設定用
電圧を前記第２の三角波電圧の平担部に加えるよ
うにしたことを特徴とする。 In order to achieve this object, the present invention provides a non-contact ignition system for an engine that determines the intersection point of a first triangular wave voltage for setting the advance angle and a second triangular wave voltage that corresponds to the rotation speed, and sets this intersection point as the ignition position. In the above, a means for generating a retard angle setting voltage according to the engine rotation speed is provided in a region where the engine rotation speed is high, and this retard angle setting voltage is applied to the flat part of the second triangular wave voltage. Features.
以下、本発明の実施例を図面を参照して詳細に
説明する。 Hereinafter, embodiments of the present invention will be described in detail with reference to the drawings.
第３図は本発明の一実施例に係る電子制御コン
デンサ充放電式点火装置のブロツク図である。こ
の図において、１は点火プラグ、２はイグニツシ
ヨンコイル、３はコンデンサ、４はサイリスタ、
５は抵抗器、６はチヤージコイル、７，８，９は
ダイオードである。コンデンサ３はチヤージコイ
ル６の出力で充電される。充電後、サイリスタ４
のゲートに正電圧が印加されると、サイリスタ４
が導通状態となり、コンデンサ３に充電された電
荷が放電されるので、この時イグニツシヨンコイ
ル２に電流が流れ、高電圧が発生して点火プラグ
１に火花が飛ぶ。即ち、点火プラグ１の点火位置
（エンジンの、ある基準位置からの回転角で表わ
す）はサイリスタ４のゲート信号によつて制御さ
れる。このサイリスタ４のゲート信号を作成する
のが第３図の下半分の回路である。 FIG. 3 is a block diagram of an electronically controlled capacitor charge/discharge type ignition device according to an embodiment of the present invention. In this figure, 1 is a spark plug, 2 is an ignition coil, 3 is a capacitor, 4 is a thyristor,
5 is a resistor, 6 is a charge coil, and 7, 8, and 9 are diodes. The capacitor 3 is charged by the output of the charge coil 6. After charging, thyristor 4
When a positive voltage is applied to the gate of thyristor 4,
becomes conductive, and the electric charge stored in the capacitor 3 is discharged. At this time, a current flows through the ignition coil 2, a high voltage is generated, and a spark flies to the spark plug 1. That is, the ignition position of the spark plug 1 (represented by the rotation angle of the engine from a certain reference position) is controlled by the gate signal of the thyristor 4. The circuit in the lower half of FIG. 3 creates the gate signal for the thyristor 4.
この回路において、１０はエンジンのクランク
シヤフトに直結されたロータで、外周に進角幅Ａ
―Ｂの角度をもつ突起１１が設けられている。１
２はロータ１０の突起１１により最小進角位置Ａ
でプラス信号、最大進角位置Ｂでマイナス信号を
発生するパルサである。１３はパルサ１２の信号
により動作するフリツプフロツプで、最大進角位
置Ｂで立ち上がり最小進角位置Ａで立ち下がる矩
形波信号を出力する。１４は第１の三角波電圧発
生回路で、フリツプフロツプ１３の出力の立ち上
がり時点Ｂから立ち下がり時点Ａまで所定の傾斜
角をもつて立ち上がる三角波電圧を発生する。１
５，１６，１７，１８は分圧抵抗器で、上記三角
波電圧に一定の進角設定用偏倚電圧V1を加え、
第１の三角波電圧Ｘ（第１図参照）を作成する。
１９は第２の三角波電圧発生回路で、フリツプフ
ロツプ１３の出力の立ち下がり時点Ａから立ち上
がり時点Ｂまで所定の傾斜角をもつて立ち上が
り、それ以後フリツプフロツプ１３の出力の立ち
下がり時点Ａまでは平担となる第２の三角波電圧
Ｙ（第１図参照）を発生する。第１、第２の三角
波電圧発生回路１４，１９としては、定電流によ
りコンデンサを充電する積分回路が用いられる。 In this circuit, 10 is a rotor that is directly connected to the engine crankshaft, and has an advance width A on its outer periphery.
- A protrusion 11 having an angle of B is provided. 1
2 is the minimum advance angle position A due to the protrusion 11 of the rotor 10.
This is a pulsar that generates a positive signal at the maximum advance angle position and a negative signal at the maximum advance angle position B. Reference numeral 13 denotes a flip-flop operated by the signal from the pulser 12, which outputs a rectangular wave signal that rises at the maximum advance angle position B and falls at the minimum advance angle position A. Reference numeral 14 denotes a first triangular wave voltage generating circuit which generates a triangular wave voltage that rises at a predetermined slope angle from time point B at which the output of the flip-flop 13 rises to time point A at which it falls. 1
5, 16, 17, and 18 are voltage dividing resistors, which add a certain lead angle setting bias voltage V 1 to the above triangular wave voltage.
A first triangular wave voltage X (see FIG. 1) is created.
Reference numeral 19 denotes a second triangular wave voltage generating circuit, in which the output of the flip-flop 13 rises with a predetermined slope angle from the falling point A to the rising point B, and thereafter remains flat until the falling point A of the output of the flip-flop 13. A second triangular wave voltage Y (see FIG. 1) is generated. As the first and second triangular wave voltage generation circuits 14 and 19, integral circuits that charge a capacitor with a constant current are used.
２０は高速域において遅角設定用電圧を発生す
る手段を構成する反転増幅器、２１，２２は反転
増幅器２０に基準電圧V3を与える分圧抵抗器で
ある。反転増幅器２０はエンジンの回転速度が高
くなつて第２の三角波電圧Ｙの平担部の電圧V2
が上記基準電圧V3より小さくなつたときに、そ
の差に応じた出力を発生するもので、その増幅度
をａとすると、その出力V4は次のようになり、
これが
V4＝−ａ（V2−V3）
遅角設定用電圧となる。２３，２４は抵抗器であ
る。 Reference numeral 20 indicates an inverting amplifier constituting means for generating a retard setting voltage in the high speed range, and 21 and 22 indicate voltage dividing resistors that provide a reference voltage V 3 to the inverting amplifier 20. The inverting amplifier 20 increases the voltage V 2 of the flat part of the second triangular wave voltage Y as the rotational speed of the engine increases.
When V becomes smaller than the reference voltage V3 , it generates an output according to the difference.If the degree of amplification is a, the output V4 is as follows,
This becomes V 4 =-a(V 2 -V 3 ) retard setting voltage. 23 and 24 are resistors.
２５は比較回路で、第１の三角波電圧Ｘと第２
の三角波電圧Ｙとを比較し、その交点を求めて点
火位置を決定する。２６は抵抗器、２７はツエナ
ダイオード、２８は始動時点火位置（最小進角位
置Ａ）の信号を供給するバイアス回路である。 25 is a comparator circuit that compares the first triangular wave voltage
The ignition position is determined by comparing the triangular wave voltage Y and finding the intersection point. 26 is a resistor, 27 is a Zener diode, and 28 is a bias circuit that supplies a signal of the starting ignition position (minimum advance position A).
次にこの回路の動作を説明する。 Next, the operation of this circuit will be explained.
ロータ１０の突起１１の回転により、パルサ１
２に、第４図イに示すように、最大進角位置Ｂお
よび最小進角位置Ａで基準信号となるパルスが発
生し、これらのパルスによりフリツプフロツプ１
３が動作して、最大進角位置Ｂで立ち上がり最小
進角位置Ａで立ち下がる矩形波信号（図示せず）
が発生する。 Due to the rotation of the protrusion 11 of the rotor 10, the pulsar 1
2, as shown in FIG.
3 is activated, and a rectangular wave signal (not shown) rises at the maximum advance angle position B and falls at the minimum advance angle position A.
occurs.
第１の三角波電圧発生回路１４では、フリツプ
フロツプ１３の信号の立ち上がり時点Ｂで積分を
開始して所定の傾斜角で電圧を立ち上げ、同信号
の立ち下がり時点Ａまで積分を継続して三角波電
圧を発生する。この三角波電圧に分圧抵抗器１５
〜１８により一定の進角設定用偏倚電圧V1を加
算したものが第１の三角波電圧Ｘ（第１図イ、第
４図ニ参照）で、これが比較回路２５の一方の入
力端子に入力される。 In the first triangular wave voltage generation circuit 14, integration is started at the rising point B of the signal from the flip-flop 13, the voltage is raised at a predetermined slope angle, and integration is continued until the falling point A of the signal to generate the triangular wave voltage. Occur. A voltage dividing resistor 15 is connected to this triangular wave voltage.
The value obtained by adding a certain advance angle setting bias voltage V 1 from 18 to 18 is the first triangular wave voltage X (see Figure 1 A and Figure 4 D), which is input to one input terminal of the comparison circuit 25 Ru.
一方、第２の三角波電圧発生回路１９では、フ
リツプフロツプ１３の信号の立ち下がり時点Ａか
ら積分を開始し、次の信号の立ち上がり時点Ｂま
で所定の傾斜角で電圧を立ち上げ、以後この値を
同信号の立ち下がり時点Ａまで保持して、第１図
イ、第４図ロに示すような第２の三角波電圧Ｙを
発生する。 On the other hand, the second triangular wave voltage generation circuit 19 starts integrating from the falling point A of the signal of the flip-flop 13, and increases the voltage at a predetermined slope angle until the rising point B of the next signal. The signal is held until the falling point A, and a second triangular wave voltage Y as shown in FIG. 1A and FIG. 4B is generated.
ところで、反転増幅器２０に与えられる基準電
圧V3は、低中速領域における第２の三角波電圧
Ｙの平担部の電圧V2より小さく設定されている
ので、低中速領域では反転増幅器２０の出力は零
レベルにある。したがつて、低中速領域では第２
の三角波電圧Ｙがそのまま比較回路２５の他方の
入力端子に入力されるので、この領域での進角特
性は先に説明したものと同じである。即ち、第５
図はこの実施例の回路の進角、遅角特性を示すも
のであるが、そのうち，，の低中速域にお
ける進角特性は、第２図の，，の低中速域
における進角特性と同じである。 By the way, the reference voltage V 3 applied to the inverting amplifier 20 is set to be lower than the voltage V 2 of the flat part of the second triangular wave voltage Y in the low-medium speed region. The output is at zero level. Therefore, in the low and medium speed range, the second
Since the triangular wave voltage Y is input as is to the other input terminal of the comparator circuit 25, the advance angle characteristics in this region are the same as those described above. That is, the fifth
The figure shows the lead angle and retard characteristics of the circuit of this embodiment. Among these, the lead angle characteristic in the low and medium speed range of , is the lead angle characteristic in the low and medium speed range of , shown in Fig. 2. is the same as
さて、高速域に入り、第４図ロに示すように、
第２の三角波電圧Ｙの平担部の電圧V2が反転増
幅器２０の基準電圧V3より小さくなると、反転
増幅器２０はその差（V2−V3）を反転増幅し、第
４図ハのような遅角設定用電圧V4を発生する。
この電圧V4は、第４図ニに示すように、第２の
三角波電圧Ｙの平担部に加算される。その結果、
比較回路２５の出力は第４図ホのようになり、こ
れがサイリスタ４のゲートに加えられるから、点
火位置Ｃは最大進角位置Ｂより遅角されたものと
なる。反転増幅器２０の出力である遅角設定用電
圧V4は、エンジン回転速度が高くなればなるほ
ど大きくなるから、回転速度の上昇にともない、
点火位置Ｃは次第に遅角され、第５図の領域の
ような遅角特性が得られる。 Now, entering the high speed range, as shown in Figure 4 B,
When the voltage V 2 of the flat part of the second triangular wave voltage Y becomes smaller than the reference voltage V 3 of the inverting amplifier 20, the inverting amplifier 20 inverts and amplifies the difference (V 2 −V 3 ), as shown in FIG. Generates the retard setting voltage V4 .
This voltage V 4 is added to the flat part of the second triangular wave voltage Y, as shown in FIG. 4D. the result,
The output of the comparison circuit 25 is as shown in FIG. 4E, and since this is applied to the gate of the thyristor 4, the ignition position C is retarded from the maximum advance position B. The retard setting voltage V4 , which is the output of the inverting amplifier 20, increases as the engine rotation speed increases, so as the rotation speed increases,
The ignition position C is gradually retarded, and a retardation characteristic like the region shown in FIG. 5 is obtained.
さらに回転速度が高くなり、第２の三角波電圧
Ｙの平担部の電圧V2に反転増幅器２０の出力V4
を加えたものが、第１の三角波電圧Ｘの最大値よ
り大きくなる領域では比較回路２５の出力は常に
零レベルとなる。したがつて、この領域では、サ
イリスタ４はパルサ１２の出力で動作するように
なり、点火位置は最小進角位置Ａに固定され、一
定である（第５図のＶ領域参照）。 As the rotation speed further increases, the voltage V 2 of the flat part of the second triangular wave voltage Y becomes the output V 4 of the inverting amplifier 20.
In the region where the sum of the values of the first triangular wave voltage X is larger than the maximum value of the first triangular wave voltage Therefore, in this region, the thyristor 4 is operated by the output of the pulsar 12, and the ignition position is fixed at the minimum advance angle position A, which is constant (see region V in FIG. 5).
このように、この実施例によれば、電子回路に
より高速域において精度の高い遅角制御を行なう
ことができる。また、高速域における遅角特性の
勾配は反転増幅器２０の増幅度ａを調節すること
によつて自由に設定することができ、しかも、遅
角を開始すべき回転速度も反転増幅器２０の基準
電圧V3を調節することによつて自由に設定する
ことができるから、任意の遅角特性を得ることが
でき、各種のエンジンに適用可能である。 In this manner, according to this embodiment, highly accurate retard control can be performed in the high speed range by the electronic circuit. Further, the gradient of the retardation characteristic in the high speed range can be freely set by adjusting the amplification degree a of the inverting amplifier 20, and the rotation speed at which the retardation should be started can also be set by the reference voltage of the inverting amplifier 20. Since it can be freely set by adjusting V3 , any retardation characteristic can be obtained, and it can be applied to various engines.
上記実施例では、遅角設定用電圧を反転増幅器
によつて得るようにしたが、この遅角設定用電圧
は高速域において回転速度に応じて大きくなる電
圧であればよいので、他の手段によつても得るこ
とができる。また、本発明は電流遮断式点火装置
にも適用可能である。 In the above embodiment, the voltage for setting the retard angle is obtained by an inverting amplifier, but since the voltage for setting the retard angle may be a voltage that increases in accordance with the rotational speed in a high-speed range, other means may be used. You can get it even if you twist it. Further, the present invention is also applicable to a current interrupt type ignition device.
以上説明したように本発明によれば、電子回路
を用いて、進角制御と共に高速域における高精度
の遅角制御を行なうことができる。 As described above, according to the present invention, it is possible to perform advance angle control as well as highly accurate retard angle control in a high speed range using an electronic circuit.
第１図イ，ロは２つの三角波電圧の組合せから
エンジン点火位置の進角制御を行なう方法を示す
波形図、第２図は第１図の方法によつて得られる
進角特性を示すグラフ、第３図は本発明の一実施
例に係るエンジン用無接点点火装置の回路図、第
４図イ〜ホは第３図の回路により高速域でエンジ
ン点火位置の遅角制御を行なう方法を示す波形
図、第５図は第３図の回路によつて得られる進
角、遅角特性を示すグラフである。
１０…ロータ、１２…パルサ、１３…フリツプ
フロツプ、１４…第１の三角波電圧発生回路、１
９…第２の三角波電圧発生回路、２０…反転増幅
器（遅角設定用電圧発生手段）、２５…比較回
路、Ｘ…第１の三角波電圧、Ｙ…第２の三角波電
圧、V1…進角設定用偏倚電圧、V2…第２の三角
波電圧Ｙの平担部の電圧、V3…基準電圧、V4…
遅角設定用電圧。
1A and 1B are waveform diagrams showing a method for controlling the advance angle of the engine ignition position from a combination of two triangular wave voltages; FIG. 2 is a graph showing the advance angle characteristics obtained by the method of FIG. 1; FIG. 3 is a circuit diagram of a contactless ignition device for an engine according to an embodiment of the present invention, and FIG. The waveform diagram of FIG. 5 is a graph showing the lead angle and retard angle characteristics obtained by the circuit of FIG. 3. 10...Rotor, 12...Pulser, 13...Flip-flop, 14...First triangular wave voltage generation circuit, 1
9... Second triangular wave voltage generation circuit, 20... Inverting amplifier (retard angle setting voltage generating means), 25... Comparison circuit, X... First triangular wave voltage, Y... Second triangular wave voltage, V 1 ... Advance angle Setting bias voltage, V 2 ... Voltage of the flat part of the second triangular wave voltage Y, V 3 ... Reference voltage, V 4 ...
Voltage for retard setting.
Claims (1)
垂直に立ち上がり、そこから最小進角位置まで所
定の傾斜角をもつて立ち上がる進角設定用の第１
の三角波電圧を発生する手段と、最小進角位置か
ら最大進角位置まで所定の傾斜角をもつて立ち上
がり、最大進角位置以後は平担となる回転速度に
応じた第２の三角波電圧を発生する手段と、前記
第１の三角波電圧と第２の三角波電圧の交点を求
める手段とを備え、この交点を点火位置とするエ
ンジン用無接点点火装置において、エンジン回転
速度が高い領域で回転速度に応じた遅角設定用電
圧を発生する手段をさらに備え、この遅角設定用
電圧を前記第２の三角波電圧の平担部に加えるよ
うにしたことを特徴とするエンジン用無接点点火
装置。 ２ 特許請求の範囲第１項において、前記遅角設
定用電圧発生手段は、ある基準電圧より前記第２
の三角波電圧の平担部の電圧が小さいときに、そ
の差に応じた電圧を発生する回路からなることを
特徴とするエンジン用無接点点火装置。[Scope of Claims] 1. A first lead angle setting device that rises vertically from the maximum advance position by the amount of bias voltage for lead angle setting, and rises from there at a predetermined inclination angle to the minimum advance position.
means for generating a triangular wave voltage, and a second triangular wave voltage corresponding to the rotational speed that rises at a predetermined slope angle from the minimum advance angle position to the maximum advance angle position and remains flat after the maximum advance angle position. and means for determining the intersection point of the first triangular wave voltage and the second triangular wave voltage, and the non-contact ignition device for an engine uses this intersection point as the ignition position. A non-contact ignition device for an engine, further comprising means for generating a corresponding retard setting voltage, the retard setting voltage being applied to a flat portion of the second triangular wave voltage. 2. In claim 1, the retard setting voltage generating means is configured to generate the second retard angle setting voltage from a certain reference voltage.
A non-contact ignition device for an engine, comprising a circuit that generates a voltage according to the difference when the voltage of the flat part of the triangular wave voltage is small.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP55122947A JPS5749070A (en) | 1980-09-06 | 1980-09-06 | Contactless ignition system for engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP55122947A JPS5749070A (en) | 1980-09-06 | 1980-09-06 | Contactless ignition system for engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5749070A JPS5749070A (en) | 1982-03-20 |
| JPS6217114B2 true JPS6217114B2 (en) | 1987-04-16 |
Family
ID=14848550
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP55122947A Granted JPS5749070A (en) | 1980-09-06 | 1980-09-06 | Contactless ignition system for engine |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS5749070A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH03124742U (en) * | 1990-03-29 | 1991-12-17 |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS58170855A (en) * | 1982-03-31 | 1983-10-07 | Honda Motor Co Ltd | Method and device for control of engine ignition timing |
| JPS59571A (en) * | 1982-06-25 | 1984-01-05 | Nippon Denso Co Ltd | Ignition angle controlling apparatus for contactless ignition device for internal-combustion engine |
| JPH0689284B2 (en) * | 1985-06-29 | 1994-11-09 | 株式会社アサヒ化学研究所 | Curable resin composition for solder-resist ink |
| JPS63238174A (en) * | 1987-03-25 | 1988-10-04 | Shikoku Chem Corp | Formation of cured coating film in resist ink composition and printed circuit board |
-
1980
- 1980-09-06 JP JP55122947A patent/JPS5749070A/en active Granted
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH03124742U (en) * | 1990-03-29 | 1991-12-17 |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS5749070A (en) | 1982-03-20 |
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